Referenced Items are not available for this document.
Closed-form expressions are derived by field calculations for the drag force exerted by spacecraft eddy current dampers. These devices are conducting slabs moving at low speed in a narrow gap between magnets with a rectangular cross section. Finite edge effects of the slab are accounted for. The results can be used for design studies.
Published in:
Aerospace and Electronic Systems, IEEE Transactions on
(Volume:AES-13
,
Issue:
2
)
Date of Publication: March 1977
- Page(s):
- 197 - 200
- ISSN :
- 0018-9251
- Digital Object Identifier :
- 10.1109/TAES.1977.308456
- Product Type:
- Journals & Magazines
- Date of Current Version :
- 20 February 2007
- Issue Date :
- March 1977
- Sponsored by :
- Aerospace & Electronic Systems Society
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